As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
POSSIBLE CRACK AT LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE AFT END (MARKED). PERFORMED ET INSPECTION OF LT ATTACH ANGLE IAW CRJ 700 NDT MANUAL PART 1, CHAPTER 51-20-006. ANGLE IS CRACKED IN RADIUS. CUT OUT DAMAGED AREA PER REO 670-55-31-015. ALL WORK DONE IAW REO 670-55-31-016 DK 7022603 1-9-7